JASC 2751
Service difficulty reports · 3,085
Reports filed under 2751 · Trailing Flap Position Indicating System, newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '2751' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '2751' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR COMA2010051050115Detector · faultyON APPROACH INTO ATL RECEIVED FLAPS FAIL CAUTION MSG AT 8 DEG. EMERGENCY DECLARED, FOLLOWED QRH A/C LANDED SAFELY. REMOVED AND REPLACED SKEW DETECTION UNIT.SDR F3LA2010043000392Warning Light · illuminatedPILOT REPORT REF LOG PAGE 508494 ITEM(S) 1 FCTL FLAP FAULT (FLIGHT CONTROL FLAP FAULT)AND ITEM 2 FCTL SLAT FAULT (FLIGHT CONTROL SLAT FAULT) EMERGENCY DECLARED. OPS TEST OF THE FLAP AND SLAT SYS OK IAW AMM 27-54-00-710-002.SDR USAA20100426SB058Indicator · faultyIAD - ON FINAL APPROACH TO DCA, CREW REPORTED A FLAP ASYMMETRY. LEFT FLAP WAS AT 16 DEGREES AND THE RIGHT FLAP WAS AT 12 DEGREES. APPROACH WAS ABORTED AND DECISION WAS MADE TO LAND AT IAD. FLAPS WERE STUCK IN SAME POSITION UNTIL HALF WAY TO IAD AND THEN RETSDR AALA20100417DFW01Pseu · defectiveDFW - CREW REPORTED LEADING EDGE SLAT ASYMMETRY LIGHT ILLUMINATED AND EICAS MESSAGE ONCE THE FLAPS WERE SET TO 20 DEGREES. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. AIRCRAFT WAS TAKEN TO AFW FOR FURTHER MAINTENANCSDR SWAA101839Sensor · faultyDIVERSION - AFTER TAKEOFF FLAPS DID NOT RAISE. FLAP LEVER WAS UP. LEFT FLAP AT POS 1 AND RT FLAP BETWEEN POS 1 & 2. WITH LED IN EXT POSITION DIVERT TO MCI. EXTEND LED USING ALT FLAP SWITCH, PER QRH. REMOVED AND REPLACED FLAP SKEW SENSOR NR 6 PER MM.SDR VNAA2010040100015Warning System · false activationON TAKEOFF FROM CLT, CREW REPORTED A SLATS FAIL MESSAGE ON FLAP RETRACTION. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. NO FAULTS WERE FOUND. AIRCRAFSDR UALA2010031900924Indicator · faultyFLAP IND SHOWS 1-2 WIDTH NEEDLE SPLIT AFTER SELECTING FLAPS 5. NO ASSOC ROLL NOTED. REPLACED FLAP INDICATOR. OPS CHECKS OKAY.SDR HALA2010031300108Indicator · stuckETOPS SIGNIFICANT SYSTEM - LT SIDE FLAP IND POINTER GOT STUCK AT 15 DEG, WHEN FLAPS GOING DOWN. TROUBLESHOT PER FIM 27-58-00/101 FIG 103. NO FAULTS FOUND. ALL OPERATIONS AND INDICATIONS NORMAL, THE SYSTEM CHECKS OK PER THE FIM.SDR TRBA2010010Indicator · malfunctionedAPPROACH INTO LAW FLAPS WOULD NOT GO TO 30 DEGREES; FLAPS BETWEEN 15 DEGREES AND 30 DEGREES. RETURNED TO DEPARTURE. R & R FLAP POSITION INDICATOR IAW JIC NR 27-55-81, BLED FLAP VALVE BLOCK, OPS CHECK GOOD.SDR UALA2010030800807Pickup · out of adjustF/CTL FLAPS LOCKED ECAM. FLT CONT FLAP LOCKED. FOUND ASSY POSITION PICKUP UNIT OUT OF ADJUSTMENT AND REPLACED. TOLERANCE IS NOW WITHIN 0.1 AT ALL FLAP SETTINGS. LIMIT IS 0.9 AT ZERO FLAPS AND 1.3 AT FLAP SETTINGS 1, 2 AND 3.SDR AALA20100227ORD01Transmitter · faultyORD - DURING APPROACH HAD A TRAILING EDGE FLAP ASSYMETRY. RAN THE QRH AND LANDED WITH FLAPS 20. ALSO HAD TRAILING EDGE FLAPS SHUTDOWN STATUS MESSAGE. FLIGHT LANDED ORD WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FLAP TRANSMITTER. SYSTEM GROSDR ASOA201000318Transmitter · intermittentSTALL FAIL CAUTION MSG IN FLIGHT NO OVERWEIGHT LANDING OCCURED ON RETURN. (EMERGENCY DECLARED AS A PRECAUTION) R & R RT FLAP POSITION TRANSMITTER REF AMM 27-55-01. OPS CK GOOD. OPS CK STALL PROTECTION, OPS CK GOOD REF AMM 27-35-01.SDR UALA2010021500571Proximity Sensor · faultedFLIGHT CONTROL ECAM MSG; FLAPS LOCKED, ALIGNMENT FAULT. HAPPENED WHEN GOING TO FLAPS-2, IAW CREW MAINT TEXT: PFR HAD FLP1 CHECK LT MECH DRIVE, FLAP 2 CHECK LT MECH DRIVE. FLAPS CHECKED OK. ECAM MESSAGES SHOW FLAP LT PROX SENSOR 2 39CV AT FAULT. MEGGERED & RASDR COMA2010020150028Warning System · activatedFLAPS FAIL CAUTION MSG AT 0 DEG DURING LANDING. EMERGENCY DECLARED, A/C LANDED SAFELY AT YUL. COMPLIED WITH TASK CARD SI-2-27I0002, FLAPS FAIL CAUTION MESSAGE FOLLOW UP MAINTENANCE ACTION.SDR CA100201003Switch · damaged(CAN) UPON FLAP RETRACTION AFTER DEPARTURE, THE NR 6 KRUGER FLAP IN TRANSIT LIGHT REMAINED ILLUMINATED. ACFT RETURNED TO BASE. THE SWITCH WAS REPLACED AND THE ACFT RETURNED TO SERVICE. (TC 20100201003)SDR COMA2010020150027Transmitter · failedON APPROACH INTO DTW RECEIVED FLAPS FAIL CAUTION MSG AT 20 DEG WITH FLAPS SELECTED TO 30 DEG. EMERGENCY DECLARED, A/C LANDED SAFELY AT DTW. REMOVED AND REPLACED LEFT FLAP POSITION TRANSMITTER.SDR UG8A2010012601Cable Assy · damagedFLAP FOLLOW UP CABLE FOUND TO HAVE OVER 50 PERCENT OF ITS DIAMETER BROKEN AT THE SWEDGED BALL.SDR SWAA100422Sensor · faultyDIVERSION - ON APPROACH TO MDW TRIED TO EXTEND FLAPS, FOR LANDING INDICATOR SHOWED SPLIT FLAPS AND WOULD NOT MOVE, RT STUCK AT 0 AND LT INDICATOR BETWEEN 1 AND 0. LANDED USING ALT FLAP METHOD. REMOVED AND REPLACED NR 4 FLAP SKEW SENSOR PER MM.SDR UALA2010012500312Indicator · faultySTATUS MSG FLAP-SLAT ELEC WHEN FLAPS SELECTED TO 5 ON TAXI. REPLACED FLAP INDICATOR. RAN FLAPS THROUGH CYCLE. OPS NOW SATISFACTORY. MESSAGE CLEARED. NEED TO ACCOMPLISH BIT TEST ON FSEU IAW MM. NO FAULTS ON BITE, REPLACED FSEU.SDR UALA2010011800207Transmitter · faultyFLAP-SLAT ELEC LIGHT INTERMITTENT ON TAXI IN. UNABLE TO VERIFY THE PROBLEMS, REPLACED FSEU AS PRECAUTION AND SYS CHECKED NORMAL. PROBLEM RECURRED. ACCOMPLISHED BITE ON FSEU AND HAD M489 FAULT. RPLC'D NR 8 FLAP POSITION TRANSMITTER. SYS CHECKS OK AT THE PRSDR UALA2010011300172Sensor · malfunctionedT/E FLAP DISAGREE ON FINAL WITH 15 FLAPS. SUGGEST CK ALL T/E FLAP ROTARY ACTUATORS FOR TRIPS. ROTARY ACTUATORS OK. BITE CHECK FSEU NO FAULTS. OPERATED FLAPS THROUGH FULL CYCLES AND OPS NORMAL. FLAP DISAGREE WAS TROUBLESHOT TO THE M548 MODULE FOR THE OTBD SDR UALA2010011100137Actuator · faultyFLAP DISAGREE MSG. FOUND "ALT FLAP PWR" CB POPPED. RE-SET AND SYS OP NORMAL. FOUND FLAP ROT ACT OVERLOAD IND ON ACT NR 1, NR 3 AND NR 8 POPPED. REPLACING ALL 3 ACT. NR 8 REPLACED. STARTING NR 1. REPLACED NR1 T-E ROTARY ACTUATOR. REPLACED NR 3 ROTARY ACTUASDR C8GA201000001Position Switch · faultyDURING CLIMB OPERATION THE NR 2 L/E FLAP AMBER LIGHT REMAINED ILLUMINATED AFTER FLAP RETRACTION. CREW PERFORMED APPROPRIATE CHECKLIST AND RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. POST FLIGHT INSP WAS PERFORMED AND THE NR 2 L/E FLAP POSITION INDISDR ASOA200901467Warning Message · illuminatedFLAP FAIL MSG AT 30 DEGREES. (EMERGENCY DECLARED - ENROUTE, ACFT DIVERTED TO DUE TO MX)SDR UHLA2009122700148Sensor · inoperativeFLAP LOW SPEED APPEARED IN CRUISE AT FL300. RAN QRH AND GOT FLAP FAIL MESSAGE. RAN QRH. DECLARED EMERGENCY. LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED T3 AND T4 SKEW SENSORS IAW EMB 170 MM 27-53-06.SDR 2009FA0001075Bellcrank · obstructedFLAP POSITION ARM BELLCRANK ASSY PN 1262060-1 HITS BRACKET ASSY PN 1262045-8 WHERE THE BRACKET ASSY ATTACHES TO SUPPORT PN 1260448-4. THE SUPPORT FLEXES WHEN HIT AND AREA HAS METAL SHAVINGS FROM THE EXCESSIVE CONTACT. SHAVINGS COULD CONTACT WIRING AND SWITCHESSDR USAA3009122193383Flap System · false indicationEMERGENCY LANDING- FLAP ASYMMETRY OCCURRED BETWEEN 10 AND 15 DEGREES WHEN FLAP 15 WAS SELECTED AN EMERGENCY WAS DECLARED AND EMERGENCY EQUIPMENT WAS DISPATCHED. THE AIRCRAFT LANDED WITHOUT INCIDENT AND TAXIED TO GATE WITHOUT ASSISTANCE. CYCLED FLAPS THRU FULSDR CALA2009122100745Transmitter · failedUPON MOVING FLAP HANDLE FROM UP POSITION FLAP INDICATOR SHOWED SPLIT (ONE NEEDLE UP, OTHER DOWN) AND YAW DAMP KICKED OFF, FOLLOWED QRH BUT WERE ONLY ABLE TO GET LED, NO TRAILING EDGE FLAPS. APPROACH AND LANDING UNREMARKABLE. SPEED 167K, MAX BRAKE GW 135K. FSDR COMA2009122150300Warning System · malfunctionedON APPROACH INTO JFK RECEIVED FLAPS FAIL CAUTION MSG. FOLLOWED QRH PROCEDURES, EMERGENCY DECLARED. A/C LANDED SAFELY IN JFK. PERFORMED FLAPS FAIL FOLLOW UP MAINTENANCE TASK CARD SI-2-2710002. OPS CHECK GOOD, NO FURTHER DEFECTS NOTED.SDR AALA20091217JFK01Indicator · faultyFLAP INDICATOR DISPLAYED A SPLIT WHEN FLAPS SELECTED TO 15, 25 AND 30 DEGREES. CREW REPORTED THAT AFTER 5 TO 10 MINUTES INDICATORS WOULD AGREE. AN ALERT 8 WAS DECLARED. NO EICAS MESSAGE OR ANNUNCIATOR LIGHTS ILLUMINATED AT ANY TIME. FOUND FLAP INDICATOR FASDR TRBA2009124Flap System · warning messageFLAP UNLOCK ON FINAL APPROACH BELOW 1,000 FT. EMERGENCY DECLARED. RESET MFC AND PERFORMED OPS TEST OF WING FLAPS AND CHECK REDUNDANCY OF MFC MODULE. TEST FACTORY IAW JIC NR 27-51-00-OPT-10040.SDR USAA20091204SB158Transmitter · out of adjustLAS - PILOT REPORTED A TRAILING EDGE SPLIT FLAP CONDITION WHEN SELECTING FLAPS 15 ON APPROACH (5 DEGREES ON ONE AND 7 DEGREES ON THE OTHER). DURING GO-AROUND, WHEN GEAR WAS SELECTED UP, SPLIT FLAP CONDITION WENT AWAY AND A FLAPS 15 LANDING WAS CONDUCTED. DURSDR AALA20091202SFO01Indicator · trippedWHILE CONFIGURING FLAP FOR LANDING FROM 5 DEGREES TO 20 DEGREES RECEIVED TRAILING EDGE FLAP DISAGREE EICAS STATUS. WENT AROUND AND FOLLOWED QRH AFTER DECLARING AN EMERGENCY. UPON COMPLETION OF QRH, RETURNED FOR FLAPS 20 DEGREE LANDING. NO OTHER ISSUES WITH SDR CA091202004Detection Sys · faulted(CAN) ON APPROACH TO MKE THE FLAPS FAILED AT ZERO DEGREES WHEN SELECTED TO 8 DEGREES. FLAP FAIL CAUTION MESSAGE DISPLAYED. AN UNEVENTFUL FLAP ZERO LANDING WAS CARRIED OUT. THE FLAPS WERE MANUALLY CONFIGURED TO 8 DEGREES BY MTC AND THE A/C FERRIED TO A MTC BSDR AALA20091130DCA01Sensor · failedINFLIGHT MIA TO DCA - CREW REPORTED A FLAP DISAGREE INDICATION PROBLEM. LANDED IAD WITHOUT INCIDENT. REPLACED NUMBER THREE FLAP SKEW SENSOR.SDR DALA1053680687Gear · inoperativeT/E FLAP TRANSMISSION GEAR REPLACED IAW EA 06-097281-03, ME02, ME04.SDR EIAA200900128Indicator · defectiveON CLIMBOUT WHEN RETRACTING FLAPS, INBOARD FLAPS STOPPED AT 2 PERCENT. WHEN ALTERNATE RETRACT WAS ATTEMPTED LJ INBOARD FLAPS DID NOT MOVE AND RESULTED IN AN ASYMMETRIC LOCKOUT. FLAPS DISCREPANCY RECTIFIED WITH NEW INDICATOR.SDR YENA20091121162Warning System · activatedFLT 904 ORD-JFK - SLAT FAIL, EICAS MESSAGE ON APPROACH TO JFK GOING FROM SLAT/FLAPS POSITION 0 TO 1, CREW RAN QRH PROCEDURE. AIRCRAFT LANDED WITHOUT INCIDENT. MX TROUBLESHOT PER TSM 27-81-00-810-802A INSPECTED LEFT AND RIGHT WING ALL 8 SLAT TORQUE LIMITER TRSDR ABXA200911180067Warning System · malfunctionedDURING APPROACH WHEN FLAPS SELECTED TO FLAPS 1 THE LEADING EDGE SLAT DISAGREE LIGHT ILLUMINATED. FOLLOWED NON NORMAL AND LANDED WITH FLAP 20. RESET SYSTEM AND OPS CKD. FLAPS AND SLATS AND PERFORMED FIM 27-51-00. FOUND NO FAULTS SYSTEM OK.SDR SIMA200929906Velocity Sensor · defectiveON FLIGHT 4472 DURING THE DESCENT THE CREW REPORTED A FLAP FAILURE MESSAGE ON EICAS. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. TROUBLESHOT SYSTEM IAW FIM 27-51-00-810-816-A AND FOUND THE LEFT VELOCITYSDR USAA2009101992796Indicator · faultyBNA - EMERGENCY LANDING - FLT 966 - FLAP DISAGREE INDICATOR. LEFT FLAP 1, RIGHT FLAP 1.75. AFTER RUNNING SHUTDOWN CHECK LIST THE FLAP INDICATOR CORRECTED TO 1 ON EACH SIDE. PILOT DECLARED EMERGENCY, EMERGENCY EQUIPMENT MET AIRCRAFT AND AIRCRAFT TAXIED TO GASDR USAA2009101492771Indicator · false indicationEMERGENCY LANDING- CAPTAIN GO A FLAP ASYMMETRICAL INDICATION BETWEEN FLAPS 5 AND 10. THE FLAPS LOCKED OUT. THE CAPTAIN STATED THE ACFT NEVER WANTED TO ROLL. THE CREW DECLARED AN EMERGENCY WITH ATC AND ATC ROLLED EMERGENCY VEHICLES TO THE RUNWAY AS A PRECAUTSDR REXA200900116Bpsu · inoperativeFLIGHT 4106 MSP/MOT - ON APPROACH TO MOT, CREW RECEIVED A "FLAP FAILURE" MESSAGE. QRH FOLLOWED AND AIR RETUNED TO MSP. MAINTENANCE TROUBLESHOT SYSTEM AND FOUND THE BRAKE POSITION SENSING UNIT (BPSU) FAILED. BPSU REMOVED AND REPLACED AND FLAPS RIGGED PER AMMSDR UALA2009101203205Transmitter · malfunctionedFLAPS FAIL TO MOVE. EICAS MESSAGE 'TE FLAP ASYM' DISPLAYED. REPLACED RIGHT TRAILING EDGE FLAP TRANSMITTER, CHECKS OKAY.SDR SWIA200922805Transmitter · false indicationUNCOMMANDED FLAP MOVEMENT AT CRUISE. (FLT 5925) REPLACED BOTH FLAP POSITION TRANSMITTERS, FDR CONFIRMED NO FLAP MOVEMENT.SDR SAJFCALS098037Sensor · failedAFTER AIRCRAFT LANDING, CREW FOUND BOTH SIDE FLAPS FAILED TO RETRACT. T/E FLAP ASYMMETRY. L IS 15, R IS 10. NR 8 FLAP SKEW SENSOR FAIL. EO 738-24-00-0017 WAS ISSUED TO INSP/PROTECT FLAP SKEW SENSOR. EO 738-27-51-0006 WAS ISSUED TO RECORD FAULT HISTORY FROMSDR UALA2009100203091Shutoff Valve · faultyFLAP SLAT ELEC STATUS MSG WILL NOT CLEAR. SLAT ISOLATION VALVE MSG ALSO. REPLACED FSEU, NO HELP. REPLACED S846, NO HELP. REPLACED FLAP-SLAT SHUTOFF VALVE MODULE. RAN FLAPS SEVERAL TIMES AND NO MSGS.SDR AALA20090929MEX01Sensor · faultedDURING APPROACH INTO MEX TRAILING EDGE FLAPS WOULD NOT EXTEND. LANDED WITHOUT INCIDENT. PERFORMED FLAP SLAT ELECTRONIC UNIT BITE FOUND NUMBER 3 FLAP SKEW SENSOR AT FAULT. REPLACED SENSOR AS PER MM 27-59-01-2, CHECKED OPN OK FOR SERVICE.SDR CALA2009092800573Sensor · failedTAKEOFF CONFIGURATION WARNING HORN SOUNDED DURING TAKEOFF AT ABOUT 50 KNOTS. TAKEOFF WAS REJECTED AT ABOUT 60 KNOTS. WARNING TEST BUTTON HAD BEEN TESTED WITH NO HORN RESULTING. AFTER REJECTION, NOTICED FLAPS WERE SPLIT L FLAP 7 R FLAP AT 5, HAD NOT NOTICED SDR IPXA09557449Transmitter · faultyINSPECTION TYPE:N/A WHEN FLAPS 15 DEG SELECTED, RECEIVED EICAS MSG "TRAILING EDGE FLAP DISAGREE". FLAP INDICATOR NEEDLES STOPPED PRIOR TO THE FLAP 15 DEG WHITE BAND. EMERGENCY DECLARED. NO SHORT IN RUN FROM NR 1 FSEA PLUG B-E/6 TO K10095 RELAY. REMOVED AND
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